Date: March 12th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


077/02:55:34 987 -0 4 0 8 0 8
N/A -0 3 -0 0 185 9
000/00:05:09 975 0 7 -0 1 180 8

080/02:40:34 908 0 0 0 6 0 6
N/A -0 5 -0 0 186 4
000/00:05:09 817 0 3 -0 1 180 4

Coasting Arc #1 (Orbit 1294)
---------------------------------------

Vector Time (GMT): 2008/070/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4596839
70                 A    =         6721751
87  meter
 Y    =        3817031
67  meter          E    =           
0002808
 Z    =       -3081854
01                 I    =           51
73235
 XDOT =      -5373
866425                 Wp   =           94
96324
 YDOT =      -2511
677784  meter/sec      RA   =          164
30377  deg
 ZDOT =       4908
303342                 TA   =          229
31408
                                          MA   =          229
33849
                                          Ha   =            186
228  n
mi
                                          Hp   =            180
939

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15081495
07                 X    =        -4624209
61
 Y    =       12523069
78  feet           Y    =         3765473
89  meter
 Z    =      -10111069
58                 Z    =        -3104252
23
 XDOT =     -17630
795357                 XDOT =       -5369
224683
 YDOT =      -8240
412677  feet/sec       YDOT =       -2571
745060  meter/sec
 ZDOT =      16103
357421                 ZDOT =        4882
208618

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19090859
27                 X    =        -5818893
90
 Y    =        4252600
88  feet           Y    =         1296192
75  meter
 Z    =      -10196419
80                 Z    =        -3107868
75
 XDOT =     -11670
546401                 XDOT =       -3557
182543
 YDOT =     -14049
161739  feet/sec       YDOT =       -4282
184498  meter/sec
 ZDOT =      16003
064003                 ZDOT =        4877
733908


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08070
46470412  
00020000  00000-0  20000-3 0  9002
2 25544  51
6387 165
2886 0002066 230
7942 129
3039 15
76185394 12952


Satellite: ISS
Catalog Number: 25544
Epoch time:      08070
46470412   =   yrday
fracday
Element set:     900
Inclination:       51
6387  deg
RA of node:       165
2886  deg
Eccentricity:     
0002066     
Arg of perigee:   230
7942  deg
Mean anomaly:     129
3039  deg
Mean motion:   15
76185394  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1295
Checksum:              296


Coasting Arc #2 (Orbit 1310)
---------------------------------------

Vector Time (GMT): 2008/071/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4201559
77                 A    =         6716333
31  meter
 Y    =        2358385
27  meter          E    =           
0008973
 Z    =       -4687552
28                 I    =           51
74195
 XDOT =      -5611
159007                 Wp   =           75
01166
 YDOT =       4475
715308  meter/sec      RA   =          159
20455  deg
 ZDOT =      -2779
728602                 TA   =          167
61736
                                          MA   =          167
59530
                                          Ha   =            186
143  n
mi
                                          Hp   =            181
023

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13784644
90                 X    =         4197646
97
 Y    =        7737484
49  feet           Y    =         2405347
37  meter
 Z    =      -15379108
53                 Z    =        -4667150
72
 XDOT =     -18409
314329                 XDOT =       -5647
286683
 YDOT =      14684
105340  feet/sec       YDOT =        4412
765967  meter/sec
 ZDOT =      -9119
844495                 ZDOT =       -2807
075642

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9014518
30                 X    =         2747625
18
 Y    =       13077874
49  feet           Y    =         3986136
14  meter
 Z    =      -15300645
06                 Z    =        -4663636
62
 XDOT =     -22006
808846                 XDOT =       -6707
675336
 YDOT =       4385
539622  feet/sec       YDOT =        1336
712477  meter/sec
 ZDOT =      -9224
088158                 ZDOT =       -2811
502071


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08071
47909596  
00020000  00000-0  20000-3 0  9015
2 25544  51
6386 160
0619 0002086 233
0607 127
0367 15
76242056 13111


Satellite: ISS
Catalog Number: 25544
Epoch time:      08071
47909596   =   yrday
fracday
Element set:     901
Inclination:       51
6386  deg
RA of node:       160
0619  deg
Eccentricity:     
0002086     
Arg of perigee:   233
0607  deg
Mean anomaly:     127
0367  deg
Mean motion:   15
76242056  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1311
Checksum:              278


Coasting Arc #3 (Orbit 1326)
---------------------------------------

Vector Time (GMT): 2008/072/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5123793
12                 A    =         6724356
83  meter
 Y    =       -3993288
52  meter          E    =           
0013287
 Z    =        1709778
29                 I    =           51
79580
 XDOT =       4224
296453                 Wp   =          122
58215
 YDOT =       2956
856225  meter/sec      RA   =          154
02385  deg
 ZDOT =      -5728
255723                 TA   =           38
51837
                                          MA   =           38
42363
                                          Ha   =            186
055  n
mi
                                          Hp   =            180
794

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16810344
88                 X    =         5159760
08
 Y    =      -13101340
28  feet           Y    =        -3935790
19  meter
 Z    =        5609508
83                 Z    =         1734757
15
 XDOT =      13859
240333                 XDOT =        4218
745299
 YDOT =       9700
971868  feet/sec       YDOT =        3004
063522  meter/sec
 ZDOT =     -18793
489904                 ZDOT =       -5707
747660

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20766550
48                 X    =         6329644
59
 Y    =       -4680341
73  feet           Y    =        -1426568
16  meter
 Z    =        5704750
99                 Z    =         1738808
10
 XDOT =       8143
207381                 XDOT =        2482
049610
 YDOT =      13222
089724  feet/sec       YDOT =        4030
092948  meter/sec
 ZDOT =     -18714
541677                 ZDOT =       -5704
192303


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08072
49345744  
00020000  00000-0  20000-3 0  9028
2 25544  51
6379 154
8353 0001899 235
2930 124
8056 15
76289555 13275


Satellite: ISS
Catalog Number: 25544
Epoch time:      08072
49345744   =   yrday
fracday
Element set:     902
Inclination:       51
6379  deg
RA of node:       154
8353  deg
Eccentricity:     
0001899     
Arg of perigee:   235
2930  deg
Mean anomaly:     124
8056  deg
Mean motion:   15
76289555  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1327
Checksum:              315


Coasting Arc #4 (Orbit 1342)
---------------------------------------

Vector Time (GMT): 2008/073/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3147918
77                 A    =         6713734
34  meter
 Y    =       -2871126
47  meter          E    =           
0003347
 Z    =        5187803
36                 I    =           51
78689
 XDOT =       6046
589649                 Wp   =          153
90566
 YDOT =      -4650
588729  meter/sec      RA   =          148
90637  deg
 ZDOT =       1091
999518                 TA   =          285
68538
                                          MA   =          285
72230
                                          Ha   =            185
952  n
mi
                                          Hp   =            180
731

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10327817
50                 X    =        -3140780
75
 Y    =       -9419706
27  feet           Y    =        -2906288
35  meter
 Z    =       17020352
24                 Z    =         5172528
18
 XDOT =      19837
892550                 XDOT =        6092
839141
 YDOT =     -15257
837037  feet/sec       YDOT =       -4582
713713  meter/sec
 ZDOT =       3582
675583                 ZDOT =        1121
486104

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5624760
53                 X    =        -1714427
01
 Y    =      -12874698
35  feet           Y    =        -3924208
06  meter
 Z    =       16961464
62                 Z    =         5169854
42
 XDOT =      23401
284250                 XDOT =        7132
711439
 YDOT =      -5341
670522  feet/sec       YDOT =       -1628
141175  meter/sec
 ZDOT =       3695
130971                 ZDOT =        1126
275920


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08073
50778597  
00020000  00000-0  20000-3 0  9038
2 25544  51
6384 149
6074 0001897 244
4094 115
6875 15
76383291 13431


Satellite: ISS
Catalog Number: 25544
Epoch time:      08073
50778597   =   yrday
fracday
Element set:     903
Inclination:       51
6384  deg
RA of node:       149
6074  deg
Eccentricity:     
0001897     
Arg of perigee:   244
4094  deg
Mean anomaly:     115
6875  deg
Mean motion:   15
76383291  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1343
Checksum:              321


Coasting Arc #5 (Orbit 1357)
---------------------------------------

Vector Time (GMT): 2008/074/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5344702
44                 A    =         6725422
23  meter
 Y    =        4070552
95  meter          E    =           
0010462
 Z    =        -156428
62                 I    =           51
85048
 XDOT =      -2992
388411                 Wp   =           39
16770
 YDOT =      -3705
010457  meter/sec      RA   =          143
75489  deg
 ZDOT =       6056
416000                 TA   =          319
13608
                                          MA   =          319
21447
                                          Ha   =            185
860  n
mi
                                          Hp   =            180
742

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17535113
00                 X    =        -5389062
87
 Y    =       13354832
51  feet           Y    =         4010537
40  meter
 Z    =        -513217
26                 Z    =         -182500
69
 XDOT =      -9817
547280                 XDOT =       -2980
156719
 YDOT =     -12155
546118  feet/sec       YDOT =       -3738
404683  meter/sec
 ZDOT =      19870
131232                 ZDOT =        6041
908804

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21385720
33                 X    =        -6518367
56
 Y    =        5326418
24  feet           Y    =         1623492
28  meter
 Z    =        -612670
96                 Z    =         -186742
11
 XDOT =      -3920
540458                 XDOT =       -1194
980732
 YDOT =     -13533
530584  feet/sec       YDOT =       -4125
020122  meter/sec
 ZDOT =      19814
083431                 ZDOT =        6039
332630


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08074
45869396  
00020000  00000-0  20000-3 0  9042
2 25544  51
6383 144
7072 0001715 254
4714 105
6261 15
76370071 13589


Satellite: ISS
Catalog Number: 25544
Epoch time:      08074
45869396   =   yrday
fracday
Element set:     904
Inclination:       51
6383  deg
RA of node:       144
7072  deg
Eccentricity:     
0001715     
Arg of perigee:   254
4714  deg
Mean anomaly:     105
6261  deg
Mean motion:   15
76370071  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1358
Checksum:              293


Coasting Arc #6 (Orbit 1373)
---------------------------------------

Vector Time (GMT): 2008/075/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2082620
82                 A    =         6713351
36  meter
 Y    =        3656613
57  meter          E    =           
0013129
 Z    =       -5242076
12                 I    =           51
83253
 XDOT =      -6126
383132                 Wp   =           98
13299
 YDOT =       4592
799916  meter/sec      RA   =          138
61088  deg
 ZDOT =        769
577401                 TA   =          179
17589
                                          MA   =          179
17372
                                          Ha   =            185
743  n
mi
                                          Hp   =            180
709

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6832745
48                 X    =         2067041
91
 Y    =       11996763
68  feet           Y    =         3679815
51  meter
 Z    =      -17198412
45                 Z    =        -5231996
74
 XDOT =     -20099
682193                 XDOT =       -6181
023623
 YDOT =      15068
241193  feet/sec       YDOT =        4523
985694  meter/sec
 ZDOT =       2524
860239                 ZDOT =         739
683133

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1853243
19                 X    =          564868
52
 Y    =       13730138
13  feet           Y    =         4184946
10  meter
 Z    =      -17159339
65                 Z    =        -5230166
72
 XDOT =     -23328
835867                 XDOT =       -7110
629172
 YDOT =       6162
523628  feet/sec       YDOT =        1878
337202  meter/sec
 ZDOT =       2410
801752                 ZDOT =         734
812374


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08075
47296543  
00020000  00000-0  20000-3 0  9054
2 25544  51
6377 139
4799 0001742 259
3776 100
7192 15
76434364 13744


Satellite: ISS
Catalog Number: 25544
Epoch time:      08075
47296543   =   yrday
fracday
Element set:     905
Inclination:       51
6377  deg
RA of node:       139
4799  deg
Eccentricity:     
0001742     
Arg of perigee:   259
3776  deg
Mean anomaly:     100
7192  deg
Mean motion:   15
76434364  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1374
Checksum:              320


Coasting Arc #7 (Orbit 1389)
---------------------------------------

Vector Time (GMT): 2008/076/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5288820
74                 A    =         6724173
72  meter
 Y    =       -3865562
97  meter          E    =           
0007774
 Z    =       -1499650
18                 I    =           51
89017
 XDOT =       1807
037706                 Wp   =          153
39925
 YDOT =       4720
610999  meter/sec      RA   =          133
49294  deg
 ZDOT =      -5813
483749                 TA   =           43
07637
                                          MA   =           43
01556
                                          Ha   =            185
746  n
mi
                                          Hp   =            180
555

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17351774
10                 X    =         5338937
89
 Y    =      -12682293
22  feet           Y    =        -3806140
17  meter
 Z    =       -4920112
14                 Z    =        -1473835
76
 XDOT =       5928
601399                 XDOT =        1782
357129
 YDOT =      15487
568893  feet/sec       YDOT =        4740
680214  meter/sec
 ZDOT =     -19073
109414                 ZDOT =       -5804
765366

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20803046
97                 X    =         6340768
72
 Y    =       -5487947
69  feet           Y    =        -1672726
46  meter
 Z    =       -4821596
83                 Z    =        -1469622
71
 XDOT =       -413
635874                 XDOT =        -126
076214
 YDOT =      15105
537247  feet/sec       YDOT =        4604
167753  meter/sec
 ZDOT =     -19039
124872                 ZDOT =       -5803
125261


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08076
48720736  
00020000  00000-0  20000-3 0  9063
2 25544  51
6373 134
2521 0001595 262
7342  97
3641 15
76484485 13906


Satellite: ISS
Catalog Number: 25544
Epoch time:      08076
48720736   =   yrday
fracday
Element set:     906
Inclination:       51
6373  deg
RA of node:       134
2521  deg
Eccentricity:     
0001595     
Arg of perigee:   262
7342  deg
Mean anomaly:      97
3641  deg
Mean motion:   15
76484485  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1390
Checksum:              301


Coasting Arc #8 (Orbit 1400)
---------------------------------------

Vector Time (GMT): 2008/077/02:58:09
975
Vector Time (MET): N/A
Weight (LBS)     : 567143
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5006354
98                 A    =         6724656
05  meter
 Y    =        4258193
06  meter          E    =           
0013101
 Z    =        1390078
01                 I    =           51
90119
 XDOT =      -2201
702014                 Wp   =           53
63503
 YDOT =      -4508
210828  meter/sec      RA   =          130
07128  deg
 ZDOT =       5850
212231                 TA   =          321
61002
                                          MA   =          321
70318
                                          Ha   =            185
936  n
mi
                                          Hp   =            180
759

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16425049
13                 X    =        -5060351
28
 Y    =       13970449
67  feet           Y    =         4201907
28  meter
 Z    =        4560623
39                 Z    =         1365626
32
 XDOT =      -7223
431804                 XDOT =       -2179
545568
 YDOT =     -14790
717941  feet/sec       YDOT =       -4532
707423  meter/sec
 ZDOT =      19193
609682                 ZDOT =        5839
570559

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4045883
81                 X    =         1233185
39
 Y    =      -21199726
07  feet           Y    =        -6461676
51  meter
 Z    =        4467373
67                 Z    =         1361655
49
 XDOT =      13443
130290                 XDOT =        4097
466112
 YDOT =       6622
851561  feet/sec       YDOT =        2018
645156  meter/sec
 ZDOT =      19152
273564                 ZDOT =        5837
612982


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08077
18448600  
00020000  00000-0  20000-3 0  9079
2 25544  51
6349 130
6555 0001833 296
9875  63
1102 15
76365468 14016


Satellite: ISS
Catalog Number: 25544
Epoch time:      08077
18448600   =   yrday
fracday
Element set:     907
Inclination:       51
6349  deg
RA of node:       130
6555  deg
Eccentricity:     
0001833     
Arg of perigee:   296
9875  deg
Mean anomaly:      63
1102  deg
Mean motion:   15
76365468  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1401
Checksum:              297


Coasting Arc #9 (Orbit 1415)
---------------------------------------

Vector Time (GMT): 2008/078/02:58:09
975
Vector Time (MET): N/A
Weight (LBS)     : 567143
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1535903
52                 A    =         6715203
89  meter
 Y    =        4417795
88  meter          E    =           
0010336
 Z    =       -4828072
35                 I    =           51
88738
 XDOT =      -5610
892678                 Wp   =          105
59419
 YDOT =       4651
697915  meter/sec      RA   =          124
90233  deg
 ZDOT =       2473
114474                 TA   =          188
50136
                                          MA   =          188
51889
                                          Ha   =            185
916  n
mi
                                          Hp   =            180
619

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5039053
53                 X    =         1509842
31
 Y    =       14494080
98  feet           Y    =         4434825
22  meter
 Z    =      -15840132
37                 Z    =        -4820674
66
 XDOT =     -18408
440544                 XDOT =       -5674
505374
 YDOT =      15261
476098  feet/sec       YDOT =        4588
598186  meter/sec
 ZDOT =       8113
892631                 ZDOT =        2445
702513

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13223986
89                 X    =        -4030671
21
 Y    =       -7842896
11  feet           Y    =        -2390514
74  meter
 Z    =      -15811242
48                 Z    =        -4819266
71
 XDOT =       3819
930249                 XDOT =        1164
314740
 YDOT =     -22576
738856  feet/sec       YDOT =       -6881
390003  meter/sec
 ZDOT =       8009
331977                 ZDOT =        2441
244386


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08078
13538502  
00020000  00000-0  20000-3 0  9087
2 25544  51
6346 125
7537 0001670 301
3260  58
7741 15
76413130 14161


Satellite: ISS
Catalog Number: 25544
Epoch time:      08078
13538502   =   yrday
fracday
Element set:     908
Inclination:       51
6346  deg
RA of node:       125
7537  deg
Eccentricity:     
0001670     
Arg of perigee:   301
3260  deg
Mean anomaly:      58
7741  deg
Mean motion:   15
76413130  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1416
Checksum:              270


Coasting Arc #10 (Orbit 1431)
---------------------------------------

Vector Time (GMT): 2008/079/02:58:09
975
Vector Time (MET): N/A
Weight (LBS)     : 567143
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4764822
28                 A    =         6721560
23  meter
 Y    =       -3756158
58  meter          E    =           
0002997
 Z    =       -2893804
47                 I    =           51
92502
 XDOT =       1357
758037                 Wp   =          108
17523
 YDOT =       5628
909437  meter/sec      RA   =          119
81061  deg
 ZDOT =      -5075
874245                 TA   =          104
97679
                                          MA   =          104
94361
                                          Ha   =            185
902  n
mi
                                          Hp   =            180
496

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15632619
02                 X    =         4820527
42
 Y    =      -12323354
93  feet           Y    =        -3702564
40  meter
 Z    =       -9494109
16                 Z    =        -2870521
76
 XDOT =       4454
586737                 XDOT =        1319
371025
 YDOT =      18467
550647  feet/sec       YDOT =        5643
877597  meter/sec
 ZDOT =     -16653
130725                 ZDOT =       -5069
372097

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3812704
29                 X    =        -1162112
27
 Y    =       19580247
98  feet           Y    =         5968059
59  meter
 Z    =       -9405271
81                 Z    =        -2866726
85
 XDOT =     -14088
162469                 XDOT =       -4294
071921
 YDOT =     -10721
984640  feet/sec       YDOT =       -3268
060918  meter/sec
 ZDOT =     -16627
529839                 ZDOT =       -5068
071095


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08079
14964761  
00020000  00000-0  20000-3 0  9090
2 25544  51
6347 120
5261 0001701 310
8657  49
2360 15
76474540 14321


Satellite: ISS
Catalog Number: 25544
Epoch time:      08079
14964761   =   yrday
fracday
Element set:     909
Inclination:       51
6347  deg
RA of node:       120
5261  deg
Eccentricity:     
0001701     
Arg of perigee:   310
8657  deg
Mean anomaly:      49
2360  deg
Mean motion:   15
76474540  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1432
Checksum:              283


Coasting Arc #11 (Orbit 1447)
---------------------------------------

Vector Time (GMT): 2008/080/02:43:09
817
Vector Time (MET): N/A
Weight (LBS)     : 567060
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4416365
07                 A    =         6714405
10  meter
 Y    =         121903
90  meter          E    =           
0003940
 Z    =        5053502
91                 I    =           51
91240
 XDOT =       1824
773626                 Wp   =          115
52982
 YDOT =      -7276
374318  meter/sec      RA   =          114
71984  deg
 ZDOT =       1767
510776                 TA   =          317
51441
                                          MA   =          317
54490
                                          Ha   =            186
380  n
mi
                                          Hp   =            180
426

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14489386
70                 X    =        -4441948
65
 Y    =         399947
19  feet           Y    =           72375
05  meter
 Z    =       16579733
95                 Z    =         5031986
36
 XDOT =       5986
790112                 XDOT =        1897
417424
 YDOT =     -23872
619152  feet/sec       YDOT =       -7255
562305  meter/sec
 ZDOT =       5798
919870                 ZDOT =        1776
552588

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11237088
15                 X    =         3425064
47
 Y    =       -9303704
05  feet           Y    =        -2835768
99  meter
 Z    =       16497236
23                 Z    =         5028357
60
 XDOT =       9347
842457                 XDOT =        2849
222381
 YDOT =      21648
867852  feet/sec       YDOT =        6598
574921  meter/sec
 ZDOT =       5832
733019                 ZDOT =        1777
817024


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08080
16388571  
00020000  00000-0  20000-3 0  9105
2 25544  51
6340 115
2971 0001640 329
7779  30
3290 15
76367860 14485


Satellite: ISS
Catalog Number: 25544
Epoch time:      08080
16388571   =   yrday
fracday
Element set:     910
Inclination:       51
6340  deg
RA of node:       115
2971  deg
Eccentricity:     
0001640     
Arg of perigee:   329
7779  deg
Mean anomaly:      30
3290  deg
Mean motion:   15
76367860  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1448
Checksum:              292


Coasting Arc #12 (Orbit 1462)
---------------------------------------

Vector Time (GMT): 2008/081/02:43:09
817
Vector Time (MET): N/A
Weight (LBS)     : 567060
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1676912
28                 A    =         6724978
16  meter
 Y    =        6463680
26  meter          E    =           
0011159
 Z    =        -746858
97                 I    =           51
96018
 XDOT =      -4791
923857                 Wp   =           32
75922
 YDOT =       -554
783244  meter/sec      RA   =          109
56419  deg
 ZDOT =       6008
453674                 TA   =          319
12756
                                          MA   =          319
21118
                                          Ha   =            186
167  n
mi
                                          Hp   =            180
258

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5501680
72                 X    =        -1745437
45
 Y    =       21206300
08  feet           Y    =         6444544
85  meter
 Z    =       -2450324
71                 Z    =         -755172
49
 XDOT =     -15721
534965                 XDOT =       -4814
551769
 YDOT =      -1820
155001  feet/sec       YDOT =        -608
495143  meter/sec
 ZDOT =      19712
774522                 ZDOT =        5985
119814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9093971
36                 X    =        -2771842
47
 Y    =      -19927916
57  feet           Y    =        -6074028
97  meter
 Z    =       -2481445
38                 Z    =         -756344
55
 XDOT =      11991
365751                 XDOT =        3654
968281
 YDOT =      -7895
281744  feet/sec       YDOT =       -2406
481875  meter/sec
 ZDOT =      19623
226614                 ZDOT =        5981
159472


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08081
11476439  
00020000  00000-0  20000-3 0  9113
2 25544  51
6343 110
3953 0001442 332
0727  28
0359 15
76443952 14638


Satellite: ISS
Catalog Number: 25544
Epoch time:      08081
11476439   =   yrday
fracday
Element set:     911
Inclination:       51
6343  deg
RA of node:       110
3953  deg
Eccentricity:     
0001442     
Arg of perigee:   332
0727  deg
Mean anomaly:      28
0359  deg
Mean motion:   15
76443952  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1463
Checksum:              273


Coasting Arc #13 (Orbit 1478)
---------------------------------------

Vector Time (GMT): 2008/082/02:43:09
817
Vector Time (MET): N/A
Weight (LBS)     : 567060
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3983429
56                 A    =         6712999
57  meter
 Y    =        1152007
24  meter          E    =           
0014673
 Z    =       -5291628
30                 I    =           51
92890
 XDOT =      -2002
431916                 Wp   =           85
85779
 YDOT =       7428
463325  meter/sec      RA   =          104
43802  deg
 ZDOT =        111
112722                 TA   =          185
18565
                                          MA   =          185
20087
                                          Ha   =            186
171  n
mi
                                          Hp   =            180
196

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13068994
63                 X    =         3995957
27
 Y    =        3779551
32  feet           Y    =         1196621
71  meter
 Z    =      -17360985
25                 Z    =        -5272246
57
 XDOT =      -6569
658516                 XDOT =       -2085
889085
 YDOT =      24371
598834  feet/sec       YDOT =        7405
604366  meter/sec
 ZDOT =        364
543051                 ZDOT =         101
181439

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12513954
52                 X    =        -3814253
34
 Y    =        5573552
17  feet           Y    =         1698818
70  meter
 Z    =      -17286523
54                 Z    =        -5268932
38
 XDOT =     -10234
523402                 XDOT =       -3119
482733
 YDOT =     -21977
009463  feet/sec       YDOT =       -6698
592484  meter/sec
 ZDOT =        327
324424                 ZDOT =          99
768485


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08082
12900656  
00020000  00000-0  20000-3 0  9129
2 25544  51
6345 105
1673 0001358 341
4238  18
6876 15
76497131 14792


Satellite: ISS
Catalog Number: 25544
Epoch time:      08082
12900656   =   yrday
fracday
Element set:     912
Inclination:       51
6345  deg
RA of node:       105
1673  deg
Eccentricity:     
0001358     
Arg of perigee:   341
4238  deg
Mean anomaly:      18
6876  deg
Mean motion:   15
76497131  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1479
Checksum:              293

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data may contain past, current and future orbital data These sources include:

NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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